Emergencies Flashcards

0
Q

ABORT START PROCEDURE

*memory item: steps

A
    1. PCL - OFF: or STARTER switch - AUTO/RESET

2. Perform Motoring Run Procedure

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1
Q

ABORT START PROCEDURE (indications)

A

~ITT rate of increase appears likely to exceed 1000 degrees C
~Normal N(sub 1) increase is haled (hung start)
~No rise i ITT is evident within 10 seconds after fuel flow indications (no start)
~Red BATT BUS warning message illuminates during the start sequence
PCL is moved or the ST READY green advisory message extinguishes during the start sequence

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2
Q

ABORT START PROCEDURE

NOTE #1

A

NOTE:
Note and report to maintenance the degree and duration of any overtemperatrue
*1. PCL - OFF; or STARTER switch - AUTO/RESET

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3
Q

ABORT START PROCEDURE

NOTE #2

A

If start is initiated with the PCL in the OFF position, abort by reselecting AUTO/RESET on the STARTER switch. If the switch is initiated with the PCL out if the OFF position but not past the IDLE gate, abort by placing the PCL to OFF
2. Perform Motoring Run Procedure

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4
Q

ABORT START (CAUTIONS)

A

If a start using external power is aborted (PMU or manual abort) do not attempt subsequent starts

Repeated PMU aborted start attempts are indicative of engine malfunction

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5
Q

MOTORING RUN PROCEDURE

A
  1. PCL - OFF
  2. IGNITION switch - NORM
  3. Propeller area - Clear
  4. STARTER switch - MANUAL for 20 seconds
  5. STARTER switch - NORM
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6
Q

FIRE WARNING ON THE GROUND

primary indications

A

illumination of the FIRE annunciators
visual smoke or fire
engine indications (high ITT, fluctuating or high fuel flow)
notification from external source
Preform engine shutdown and Egress if applicable

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7
Q

EMERGENCY ENGINE SHUTDOWN ON THE GROUND*

memory item

A
    1. PCL - OFF
    1. FIREWALL SHUTOFF HANDLE - PULL
  • 3 Emergency ground egress - As required
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8
Q

EMERGENCY GROUND EGRESS*

memory item

A
    1. ISS mode selector - SOLO
    1. Seat safety pin - Install (BOTH)
    1. PARKING BREAK - As required
    1. Canopy - Open

IF THE CAOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS

    1. CFS handle - Rotate and pull (BOTH)
    1. Upper fittings, lower fittings, and leg restraint garters -Release (BOTH)
    1. BAT, GEN, and AUX BAT switches - OFF
    1. Evacuate aircraft
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9
Q

TAKEOFF EMERGENCIES
(ABORT)
(*memory item)

A
    1. PCL - IDLE
    1. BRAKES - AS REQUIRED

WARNING
After a stop which required maximum effort braking and if overheated brakes are suspected, do not taxi into or park in a congested area until brakes have had sufficient time to cool. Do not set parking brake.

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10
Q

ENGINE FAILURE IMMEDIATELY AFTER TAEOFF (SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD)
(*memory item)
(WARNINGS)

A

If insufficient runway remains to land straight ahead, consider immediate ejection

Do not sacrifice aircraft control while troubleshooting or lowering gear with emergency system

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11
Q

ENGINE FAILURE IMMEDIATELY AFTER TAEOFF (SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD)
(*memory item)

A

*1. AIRSPEED - 110 KNOTS (MINIMUM)
*2. PCL - AS REQUIRED
Note
The pilot should select IDLE to use the increased drag of the not yet feathered propeller or select OFF to reduce the sink rate

*3. EMER LDG GR HANDLE - PULL
Note: with a loss of hydrauic pressure, landing gear and flaps cannot be lowered by normal means

*4. Flaps - As required

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12
Q

PMU OFF GROUND START

A
  1. Canopy - CLOSED AND LOCKED
  2. Navigation and anti-collision lights - A/R (as required)
  3. PMU switch - OFF (VERIFY PMU FAIL WARNING AND PMU STATUS CAUTION MESSAGES ILLUMINATE)
    b. FIREWALL SHUTOFF handle - Down
  4. BLEED AIR INFLOW switch - OFF
  5. BOOST PUMP switch - ON
  6. IGNITION switch - ON
  7. Propeller area - CLEAR
  8. STARTER switch - MANUAL
  9. PCL - at 13% N(1), MINIMUM, ADVANCE TO OBTAIN FUEL FLOW INDICATIONS (EXPECT APPROX. 70 TO 80 PPH)
  10. ITT, N(1),- Monitor
  11. Oil and hydraulic pressure - CHECK
  12. PCL - ADVANCE SLOWLY TO REACH IDLE AT APPROX. 67% N(1)
  13. STARTER switch - NORM
  14. IGNITION switch - NORM
  15. BOOST PUMP switch - ARM
  16. External Power - DISCONNECT (IF USED) AND DOOR SECURED
  17. GEN switch - ON,
  18. BLEED AIR INFLOW switch - NORM
  19. Before Taxi Checklist - PERFORM
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14
Q

CONTROLLED EJECTION

A

Perform as time and conditions permit

  1. Notify crewmember of decision to eject (BOTH)
  2. Altitude - 2000 FEET AGL MIN (RECOMMENDED)
  3. Airspeed - 125-180 KIAS (RECOMMENDED)
  4. Distress call - TRANSMIT
  5. Transponder - 7700
  6. Loose equipment - STOW (BOTH)
  7. Visor - DOWN (BOTH)
  8. Oxygen mask and helmet - FASTENED AND TIGHT, CHIN STRAP FASTENED (BOTH)
  9. Leg restraint garters - CHECK (BOTH)
  10. Harness - LOCKED (BOTH)
  11. SSK deployment knob - A/R (BOTH)
  12. Turn aircraft toward uninhabited area
  13. PCL - OFF
  14. Assume proper position:
    a. Head back firmly against headpad
    b. Shoulders and back against seat back
    c. Elbows close to body
    d. Legs flat on seat pad
    e. Legs extended, but not rigid
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15
Q

EJECT

A

*1. EJECTION HANDLE - PULL (BOTH)

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16
Q

PMU FAULT

on the ground

A
  1. PMU switch - OFF, THEN NORM

if PMU STATUS caution remains illuminated, confirm source of fault prior to flight

17
Q

BARRIER ENGAGEMENT

A

Aircrews will not cal for a raised barrier in the event of an aborted takeoff. If a raised barrie is already up, aircrews will steer around it, to include departing the prepared surface if necessary, or ejecting before engagment